DUMMY CUBESAT, 52983
Orbit data source: Space-Track
DUMMY CUBESAT, 52983 is a payload satellite owned by KARI (KR) in SSO that was launched on Tue, 21 Jun 2022 UTC via an NURI launch vehicle from the Naro Space Center, South Korea (NSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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52983 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
KARI
Mission
Non-operational Civil Technology
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 DUMMY CUBESAT
1 52983U 22065H 26171.32157197 .00000257 00000-0 62454-4 0 9993
2 52983 98.2288 312.4381 0008013 23.7902 336.3667 14.60598681210604Epoch: 2026-06-20T07:43Z
TLE epoch observation values (Epoch: 2026-06-20T07:43:03.818Z)
Latitude
-0.00003°
Longitude
-71.86567°
Altitude
689.037 km
Speed
7.515 km/s
True Right ascension
20h 49m 45s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:50:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
693.986 km
Perigee altitude
682.661 km
Semi-major axis
7,066.46 km
Eccentricity
0.0008
Inclination
98.2288°
RAAN
312.4381°
Arg. of periapsis
23.7902°
True anomaly
336.32986°
Mean anomaly
336.3667°
Eccentric anomaly
336.34828°
Mean motion
3.65376 °/min
Orbital period
98.53 mins
BSTAR
0.000062454
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Other satellites on launch #65 in the year 2022 (2022-06-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DUMMY CUBESAT Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 21:09:02.258Z | 55.526° ENE | 2026-06-22 21:12:02.258Z | 96.578° ESE | 15.604° | 2026-06-22 21:14:02.258Z | 124.204° SE |
| 7 mins | 2026-06-22 22:46:02.258Z | 357.061° N | 2026-06-22 22:49:02.258Z | 307.913° NW | 36.016° | 2026-06-22 22:53:02.258Z | 218.175° SW |
| 4 mins | 2026-06-23 08:14:02.258Z | 91.69° ESE | 2026-06-23 08:16:02.258Z | 61.834° ENE | 16.277° | 2026-06-23 08:18:02.258Z | 33.15° NE |
| 7 mins | 2026-06-23 09:50:02.258Z | 192.675° SSW | 2026-06-23 09:53:02.258Z | 262.434° W | 37.098° | 2026-06-23 09:57:02.258Z | 333.926° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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